View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 69009U 26145.46041912 +.00000000 +00000-0 +53702-3 0 00002
2 69009 97.4066 43.6664 0006750 69.9365 290.2596 15.19645788 00
| Epoch (UTC): | 25 May 2026 11:03:00 |
| Eccentricity: | 0.0006750 |
| inclination: | 97.4066° |
| perigee height: | 502 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 43.6664° |
| argument of perigee: | 69.9365° |
| revolutions per day: | 15.19645788 |
| mean anomaly at epoch: | 290.2596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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